JP4316076B2 - Composite parts repair equipment - Google Patents

Composite parts repair equipment Download PDF

Info

Publication number
JP4316076B2
JP4316076B2 JP31388399A JP31388399A JP4316076B2 JP 4316076 B2 JP4316076 B2 JP 4316076B2 JP 31388399 A JP31388399 A JP 31388399A JP 31388399 A JP31388399 A JP 31388399A JP 4316076 B2 JP4316076 B2 JP 4316076B2
Authority
JP
Japan
Prior art keywords
repair
cylindrical portion
heat
composite
composite material
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
JP31388399A
Other languages
Japanese (ja)
Other versions
JP2001129891A (en
Inventor
島 正 憲 中
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Subaru Corp
Original Assignee
Fuji Jukogyo KK
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Fuji Jukogyo KK filed Critical Fuji Jukogyo KK
Priority to JP31388399A priority Critical patent/JP4316076B2/en
Publication of JP2001129891A publication Critical patent/JP2001129891A/en
Application granted granted Critical
Publication of JP4316076B2 publication Critical patent/JP4316076B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Images

Description

【0001】
【発明の属する技術分野】
本発明は、修理パッチのレイアップおよびバギング作業を容易に行うとともに、修理に供した部材の再利用化を図るようにした複合材部品修理装置に関する。
【0002】
【従来の技術】
従来の複合材部品の修理パッチを硬化する複合材部品修理装置の一例を図6に示す。図6に示す複合材部品修理装置1は、複合材部品2の修理部位2aに設けられた修理パッチ3を覆うように配置された真空バッグ材4と、この真空バッグ材4の周囲に設けられて修理パッチ3を含む複合材部品2と真空バッグ材4の間に密封空間5を形成するシーラント材6と、真空バッグ材4内の密封空間5に配置されたヒートブランケット7と、このヒートブランケット7の上側に配置されたブリーザ8と、ヒートブランケット7の下側に配置されたブリーダ材9を有する。
【0003】
上記複合材部品修理装置1を用いて複合材部品2の修理部位2aを修理するには、まず、複合材部品2の修理部位2aに相当する部分を除去し、複合材部品2の修理部位2aに接着剤を介してプリプレグ修理パッチ3をセットする。
【0004】
つぎに、修理しようとする複合材部品2の上に孔あき離型フィルム10を配置す、孔あき離型フィルム10の上にブリーダ材9を配置し、ブリーダ材9の上にエッジブリーザ11,11および離型フィルム12を介してヒートブランケット7を配置し、ヒートブランケット7の上にブリーザ8を配置する。
【0005】
つぎに、これら全体を真空バッグ材4で覆い、真空バッグ材4の周囲に配置されたシーラント材6により複合材部品2と真空バッグ材3の間に密封空間5を形成する。
【0006】
つぎに、密封空間5を図示しない真空装置により真空引きし、ヒートブランケット7に埋設された熱線に通電してヒートブランケット7を加熱する。このヒートブランケット7の加熱はヒートブランケット7に接続されたヒートブランケット制御器13により制御される。ヒートブランケット制御器13により制御されたヒートブランケット7の発熱量により修理パッチ3が加熱硬化され、修理パッチ3は複合材部品2の修理部位2aに結合される。これにより、複合材部品2の修理が終了する。
【0007】
【発明が解決しようとする課題】
従来の複合材部品修理装置は、真空バッグ材、ブリーザ、離型フィルム、ブリーダ材およびシーラント材を含む多種多様の副資材を必要としているため、修理パッチのレイアップおよびバギング作業が煩雑になり、また、修理部位の曲面形状が小さな曲げを含む場合、ヒートブランケットをこの修理部位の曲面形状に合わせた形状に保持することが難しく、修理部位に真空圧が十分加わらないために、複合材部品の修理部の品質が悪くなってしまうという問題点がある。
【0008】
また、従来の複合材部品修理装置では、複合材部品の修理の際に、ほとんどの副資材にプリプレグ材の樹脂が付着してしまうため、修理に供したほとんどの副資材を再利用することなく廃棄処分するので、修理後の廃棄物が多くなるという問題点もある。
【0009】
本発明は上記した点に鑑みてなされたもので、修理パッチのレイアップおよびバギング作業が容易でかつ修理後の廃棄物も少なくなる複合材部品修理装置を提供することを目的とする。
【0010】
【課題を解決するための手段】
本発明の複合材部品修理装置は、装置本体の筒状部の一端側の開口を耐熱性伸縮シートにより閉鎖し、耐熱性伸縮シートを囲むように設けられたシール材により装置本体と複合材部品との間に密封空間を形成し、この密封空間を装置本体に形成された空気通路に連通し、筒状部に液体を収容し、この液体を加熱装置により加熱し、密封空間を真空引きすることで、耐熱性伸縮シートを複合材部品の修理部位に密着させ、加熱装置により加熱された液体により複合材部品の修理部位に設けられた修理パッチを加熱硬化して修理パッチを複合材部品の修理部位に一体結合することで複合材部品の修理を行なう。
【0011】
【発明の実施の形態】
以下本発明の実施の形態を図面を参照して説明する。
【0012】
図1において符号20は本発明による複合材部品修理装置を示し、この複合材部品修理装置20は、フレーム21と筒状部22とを備えた装置本体23を有する。
【0013】
上記フレーム21は、全体形状が上面からみて円形または矩形であり、その中央部に上下を開口した空間24を有する。この空間24は上端から下端まで内方に傾斜した傾斜面を有する周壁25により形成される。この周壁25には空気通路26が形成されている。空気通路26は、一端を空間24に連通し他端を図示しない接続パイプに接続されている。この接続パイプは図示しない真空装置に接続される。フレーム21の下面全周には空間24を囲むように連続した紐状シリコンシール材27が配置されている。
【0014】
上記筒状部22は、下端に半径方向外方に延びるフランジ部28を有する。このフランジ部28の下面に耐熱性伸縮シート29が配置されている。筒状部22は、フランジ部28を耐熱性伸縮シート29を介してフレーム21の上面に形成された支持部30に載置され、図示しない固定手段によりフレーム21に取り付けられる。筒状部22の下端開口は耐熱性伸縮シート29により閉じられることで筒状部22の内部に液体収容空間31が形成される。この液体収容空間31に液体32が収容される。この液体32は、180℃以上の温度に加熱されることがあるので、引火温度が300℃より高い特性を有するシリコンオイルであることが望ましい。また、筒状部22の内部に液体32を加熱するための加熱装置33が上下方向に移動自在に配置されている。この加熱装置33は筒状の通路を閉塞して移動できるようにシリコンシール材34を介して筒状部22の内面に取付けられている。加熱装置33はヒータ35を有し、ヒータ35は配線36を介してヒータ制御器37に接続されている。
【0015】
さらに、筒状部22の内部には、液体収容部31の液体32に検出部38aが埋没するように熱電対のような温度計38が配置されている。この温度計38により検出された液体32の温度検出信号はヒータ制御器37に送られ、このヒータ制御器37から発する制御信号により加熱装置33のヒータ35の温度が制御される。
【0016】
上記複合材部品修理装置20は、図2に示すように、孔あき離型フィルム10およびブリーダ材9を介在して複合材部品2の損傷部2aの上に配置され、空気通路26を図示しない接続パイプを介して真空装置に接続する。
【0017】
つぎに、本発明の複合材部品修理装置20の作用を図2ないし図5を参照して説明する。
【0018】
複合材部品2の損傷部位の修理準備段階として、複合材部品2の修理部位2aに相当する損傷部を複合材部品2から除去し、複合材部品2の修理部位2aの表面処理を行ない、修理部位2aにプリプレグ修理パッチ3を接着剤を介してセットする。
【0019】
つぎに、プリプレグ修理パッチ3を含む複合材部品2の上に、図2に示すように、孔あき離型フィルム10およびブリーダ材9を配置し、その上に複合材部品修理装置20を図3に示すように配置する。この段階においては、空気通路26は大気に連通し、空間24は大気圧と同じであり、耐熱性伸縮シート29は筒状部22の下端開口を閉鎖した水平位置にある。
【0020】
つぎに、空気通路26を図示しない接続パイプを介して真空装置に接続し、真空装置を作動させると、図4に示すように、空間24の空気の真空引きが開始され、空間24の空気圧は低圧状態となり、耐熱性伸縮シート29は、図3に示す位置から図4に示す位置まで中央部分が下方に伸びる。これにより、筒状部22の液体収容空間31に収容されたシリコンオイル32も下方に移動するが、耐熱性伸縮シート29は、全周囲が筒状部22のフランジ部28とフレーム21の支持部30によりシール結合されているので、シリコンオイル32が耐熱性伸縮シート29の伸縮により外部に漏れ出ることはない。
【0021】
さらに、真空装置の作動を続けると、空間24の空気がさらに真空引きされ、図5に示すように、空間24空気圧は真空状態となり、耐熱性伸縮シート29は、具有する伸縮性により中央部分がさらに下方に伸び、プリプレグ修理パッチ3を含む複合材部品2の上に密着する。
【0022】
つぎに、ヒータ制御器37を作動させると、筒状部22の内部に配置された加熱装置33のヒータ35が発熱し、ヒータ35から発する熱で、筒状部22の液体収容空間31に収容されたシリコンオイル32が、プリプレグ修理パッチ3を硬化するのに必要な120℃以上の温度に加熱される。耐熱性伸縮シート29は、プリプレグ修理パッチ3を含む複合材部品2の上に密着しているので、シリコンオイル32の熱は、プリプレグ修理パッチ3を硬化温度以上に加熱し、プリプレグ修理パッチ3を硬化させる。これにより、プリプレグ修理パッチ3は、複合材部品2の修理部位2aに一体的に結合され、複合材部品2の修理が終了する。
【0023】
複合材部品2を修理した後の複合材部品修理装置20は、ヒータ制御器37の作動を止めることでシリコンオイル32の温度が下げられ、真空装置の作動を止めることで図3に示す状態に戻される。
【0024】
【発明の効果】
以上述べたように本発明によれば、筒状部の開口端を閉鎖する耐熱性伸縮シートを真空引によって修理パッチを含む複合材部品に密着させ、筒状部に収容された液体の熱で修理パッチを加熱硬化させるようにしたので、修理パッチのレイアップおよびバギング作業が簡単になり、修理部位の曲面形状が小さな曲げ半径を含む場合でも、耐熱性伸縮シートートを修理部位の曲面形状に合わせた形状に保持することができ、修理部位に真空圧が十分加わるので、複合材部品の修理部の品質がよくなり、しかも、修理後の廃棄物も少なくなるという効果を奏する。
【図面の簡単な説明】
【図1】本発明による複合材部品修理装置の断面図。
【図2】本発明による複合材部品修理装置の使用状態を示す図。
【図3】本発明による複合材部品修理装置を修理しようとする複合材部品に設置した状態を示す図。
【図4】図3に示す複合材部品修理装置の密封空間から空気の一部を真空引きした状態を示す図。
【図5】図3に示す複合材部品修理装置の密封空間から空気を完全に真空引きした状態を示す図。
【図6】従来の複合材部品修理装置を示す図。
【符号の説明】
20 複合材部品修理装置
21 フレーム
22 筒状部
23 装置本体
24 空間
26 空気通路
27 シリコンシール材
29 耐熱性伸縮シート
31 液体収容空間
32 液体
33 加熱装置
[0001]
BACKGROUND OF THE INVENTION
The present invention relates to a composite material parts repairing apparatus that facilitates layup and bagging work of repair patches, and enables reuse of members used for repair.
[0002]
[Prior art]
FIG. 6 shows an example of a composite part repair device for curing a repair patch for a conventional composite part. The composite material part repair device 1 shown in FIG. 6 is provided around the vacuum bag material 4 and the vacuum bag material 4 arranged so as to cover the repair patch 3 provided at the repair site 2 a of the composite material part 2. A sealant material 6 that forms a sealed space 5 between the composite part 2 including the repair patch 3 and the vacuum bag material 4, a heat blanket 7 disposed in the sealed space 5 in the vacuum bag material 4, and this heat blanket 7 and a bleeder material 9 disposed below the heat blanket 7.
[0003]
In order to repair the repair part 2a of the composite material part 2 using the composite material part repairing apparatus 1, first, the part corresponding to the repair part 2a of the composite material part 2 is removed, and the repair part 2a of the composite material part 2 is removed. The prepreg repair patch 3 is set on the adhesive.
[0004]
Next, the perforated release film 10 is disposed on the composite material part 2 to be repaired, the bleeder material 9 is disposed on the perforated release film 10, and the edge breather 11, 11 and the release film 12, the heat blanket 7 is disposed, and the breather 8 is disposed on the heat blanket 7.
[0005]
Next, the whole is covered with the vacuum bag material 4, and the sealed space 5 is formed between the composite material component 2 and the vacuum bag material 3 by the sealant material 6 disposed around the vacuum bag material 4.
[0006]
Next, the sealed space 5 is evacuated by a vacuum device (not shown), and the heat blanket 7 is heated by energizing the heat wire embedded in the heat blanket 7. Heating of the heat blanket 7 is controlled by a heat blanket controller 13 connected to the heat blanket 7. The repair patch 3 is heated and cured by the amount of heat generated by the heat blanket 7 controlled by the heat blanket controller 13, and the repair patch 3 is coupled to the repair site 2 a of the composite part 2. Thereby, the repair of the composite material part 2 is completed.
[0007]
[Problems to be solved by the invention]
Conventional composite parts repair devices require a wide variety of secondary materials including vacuum bag materials, breathers, release films, bleeder materials and sealant materials, making repair patch layup and bagging work complicated. In addition, when the curved shape of the repaired part includes a small bend, it is difficult to hold the heat blanket in a shape that matches the curved shape of the repaired part, and a sufficient vacuum pressure is not applied to the repaired part. There is a problem that the quality of the repair department deteriorates.
[0008]
Also, in the conventional composite parts repair equipment, when repairing composite parts, the resin of the prepreg material adheres to most secondary materials, so most of the secondary materials used for repair are not reused. Since it is disposed of, there is a problem that the waste after repair increases.
[0009]
The present invention has been made in view of the above points, and an object of the present invention is to provide a composite part repairing apparatus that facilitates repair patch lay-up and bagging and reduces the amount of waste after repair.
[0010]
[Means for Solving the Problems]
The composite material part repairing apparatus of the present invention is such that the opening on one end side of the cylindrical portion of the apparatus main body is closed with a heat resistant elastic sheet, and the apparatus main body and the composite material part are provided by a sealing material provided so as to surround the heat resistant elastic sheet. A sealed space is formed between the air passage and the air passage formed in the main body of the apparatus, the liquid is stored in the cylindrical portion, the liquid is heated by the heating device, and the sealed space is evacuated. Thus, the heat-resistant elastic sheet is brought into close contact with the repaired part of the composite part, and the repair patch provided at the repaired part of the composite part is heated and cured by the liquid heated by the heating device to fix the repair patch to the composite part. Repair composite parts by connecting them to the repair site.
[0011]
DETAILED DESCRIPTION OF THE INVENTION
Embodiments of the present invention will be described below with reference to the drawings.
[0012]
In FIG. 1, reference numeral 20 denotes a composite part repairing device according to the present invention, and this composite part repairing device 20 includes a device main body 23 having a frame 21 and a cylindrical portion 22.
[0013]
The frame 21 has a circular shape or a rectangular shape as viewed from above, and has a space 24 that opens upward and downward in the center. The space 24 is formed by a peripheral wall 25 having an inclined surface inclined inward from the upper end to the lower end. An air passage 26 is formed in the peripheral wall 25. The air passage 26 has one end communicating with the space 24 and the other end connected to a connection pipe (not shown). This connection pipe is connected to a vacuum device (not shown). A continuous string-like silicon seal material 27 is disposed around the entire lower surface of the frame 21 so as to surround the space 24.
[0014]
The cylindrical portion 22 has a flange portion 28 extending radially outward at the lower end. A heat resistant elastic sheet 29 is disposed on the lower surface of the flange portion 28. The cylindrical portion 22 is mounted on the support portion 30 formed on the upper surface of the frame 21 with the flange portion 28 interposed between the heat resistant elastic sheet 29 and attached to the frame 21 by a fixing means (not shown). The lower end opening of the cylindrical part 22 is closed by a heat-resistant elastic sheet 29, thereby forming a liquid storage space 31 inside the cylindrical part 22. A liquid 32 is stored in the liquid storage space 31. Since the liquid 32 may be heated to a temperature of 180 ° C. or higher, it is desirable that the liquid 32 is silicon oil having a characteristic that the flash temperature is higher than 300 ° C. Further, a heating device 33 for heating the liquid 32 is disposed in the cylindrical portion 22 so as to be movable in the vertical direction. The heating device 33 is attached to the inner surface of the cylindrical portion 22 via a silicon seal material 34 so as to be able to move while closing the cylindrical passage. The heating device 33 has a heater 35, and the heater 35 is connected to a heater controller 37 via a wiring 36.
[0015]
Furthermore, a thermometer 38 such as a thermocouple is disposed inside the cylindrical portion 22 so that the detection portion 38a is buried in the liquid 32 of the liquid storage portion 31. The temperature detection signal of the liquid 32 detected by the thermometer 38 is sent to the heater controller 37, and the temperature of the heater 35 of the heating device 33 is controlled by a control signal generated from the heater controller 37.
[0016]
As shown in FIG. 2, the composite part repairing device 20 is disposed on the damaged part 2a of the composite part 2 with the perforated release film 10 and the bleeder material 9 interposed therebetween, and the air passage 26 is not shown. Connect to the vacuum device via a connecting pipe.
[0017]
Next, the operation of the composite part repairing apparatus 20 of the present invention will be described with reference to FIGS.
[0018]
As a repair preparation stage of the damaged part of the composite material part 2, the damaged part corresponding to the repaired part 2a of the composite material part 2 is removed from the composite material part 2, and the repaired part 2a of the composite material part 2 is subjected to surface treatment and repaired. The prepreg repair patch 3 is set on the part 2a via an adhesive.
[0019]
Next, as shown in FIG. 2, a perforated release film 10 and a bleeder material 9 are arranged on the composite material part 2 including the prepreg repair patch 3, and the composite material part repair device 20 is arranged on the composite material part repair device 20. Arrange as shown. At this stage, the air passage 26 communicates with the atmosphere, the space 24 is the same as the atmospheric pressure, and the heat-resistant stretchable sheet 29 is in a horizontal position where the lower end opening of the cylindrical portion 22 is closed.
[0020]
Next, when the air passage 26 is connected to a vacuum device via a connection pipe (not shown) and the vacuum device is operated, evacuation of the air in the space 24 is started, as shown in FIG. The low-pressure state is established, and the heat-resistant stretchable sheet 29 extends downward from the position shown in FIG. 3 to the position shown in FIG. As a result, the silicon oil 32 accommodated in the liquid accommodating space 31 of the cylindrical portion 22 also moves downward, but the heat resistant stretchable sheet 29 is entirely supported by the flange portion 28 of the cylindrical portion 22 and the support portion of the frame 21. Since the seal bonding is performed by 30, the silicon oil 32 does not leak to the outside due to the expansion and contraction of the heat-resistant elastic sheet 29.
[0021]
Further, when the operation of the vacuum device is continued, the air in the space 24 is further evacuated, and as shown in FIG. 5, the air pressure in the space 24 is in a vacuum state. It extends further downward and adheres onto the composite material part 2 including the prepreg repair patch 3.
[0022]
Next, when the heater controller 37 is operated, the heater 35 of the heating device 33 arranged inside the cylindrical portion 22 generates heat, and is stored in the liquid storage space 31 of the cylindrical portion 22 by the heat generated from the heater 35. The silicon oil 32 thus heated is heated to a temperature of 120 ° C. or higher necessary for curing the prepreg repair patch 3. Since the heat-resistant elastic sheet 29 is in close contact with the composite material part 2 including the prepreg repair patch 3, the heat of the silicone oil 32 heats the prepreg repair patch 3 to a curing temperature or higher, Harden. Thereby, the prepreg repair patch 3 is integrally coupled to the repair site 2a of the composite material part 2, and the repair of the composite material part 2 is completed.
[0023]
After the composite material part 2 is repaired, the composite material part repair device 20 is brought into the state shown in FIG. 3 by stopping the operation of the heater controller 37 to lower the temperature of the silicon oil 32 and stopping the operation of the vacuum device. Returned.
[0024]
【The invention's effect】
As described above, according to the present invention, the heat-resistant elastic sheet that closes the open end of the cylindrical portion is brought into close contact with the composite part including the repair patch by vacuum drawing, and the heat of the liquid contained in the cylindrical portion is used. The repair patch is heat-cured, making repair patch lay-up and bagging easier, and even if the curved surface of the repair site contains a small bending radius, the heat-resistant elastic sheet is matched to the curved shape of the repair site. Since the vacuum pressure is sufficiently applied to the repair site, the quality of the repair part of the composite material part is improved, and the waste after repair is reduced.
[Brief description of the drawings]
FIG. 1 is a cross-sectional view of a composite part repair device according to the present invention.
FIG. 2 is a diagram showing a use state of a composite material parts repair device according to the present invention.
FIG. 3 is a view showing a state in which the composite material repair device according to the present invention is installed in a composite material to be repaired.
4 is a view showing a state in which a part of air is evacuated from the sealed space of the composite part repairing apparatus shown in FIG. 3;
5 is a view showing a state in which air is completely evacuated from the sealed space of the composite part repairing device shown in FIG. 3;
FIG. 6 is a view showing a conventional composite material parts repair device.
[Explanation of symbols]
20 Composite material parts repair device 21 Frame 22 Cylindrical portion 23 Device body 24 Space 26 Air passage 27 Silicon seal material 29 Heat-resistant elastic sheet 31 Liquid storage space 32 Liquid 33 Heating device

Claims (4)

両端が開口した筒状部を有する装置本体と、装置本体の筒状部の一端を閉鎖する耐熱性伸縮シートと、装置本体の上記一端側の端面に耐熱性伸縮シートを囲むように設けられたシール材と、装置本体に形成されシール材に囲まれた空間に通じる空気通路と、筒状部に収容された液体と、筒状部の内部に配置され収容された液体を加熱する加熱装置とを有することを特徴とする複合材部品修理装置。An apparatus main body having a cylindrical portion that is open at both ends, a heat-resistant elastic sheet that closes one end of the cylindrical portion of the apparatus main body, and a heat-resistant elastic sheet that surrounds the end surface on the one end side of the apparatus main body. A sealing material, an air passage that is formed in the apparatus main body and communicates with a space surrounded by the sealing material, a liquid contained in the cylindrical portion, and a heating device that heats the liquid that is disposed inside the cylindrical portion and accommodated An apparatus for repairing composite material parts, comprising: 上記液体がシリコンオイルであることを特徴とする請求項1に記載の複合材部品修理装置。2. The composite part repairing apparatus according to claim 1, wherein the liquid is silicon oil. 装置本体の空気通路に接続され空気を吸引する吸引装置を有することを特徴とする請求項1に記載の複合材部品修理装置。The composite part repairing device according to claim 1, further comprising a suction device that is connected to an air passage of the device main body and sucks air. 加熱装置は筒状部の他端側を密封するとともに内面に沿って移動自在に配置されていることを特徴とする請求項1に記載の複合材部品修理装置。2. The composite part repairing device according to claim 1, wherein the heating device seals the other end side of the cylindrical portion and is movably disposed along the inner surface.
JP31388399A 1999-11-04 1999-11-04 Composite parts repair equipment Expired - Fee Related JP4316076B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP31388399A JP4316076B2 (en) 1999-11-04 1999-11-04 Composite parts repair equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP31388399A JP4316076B2 (en) 1999-11-04 1999-11-04 Composite parts repair equipment

Publications (2)

Publication Number Publication Date
JP2001129891A JP2001129891A (en) 2001-05-15
JP4316076B2 true JP4316076B2 (en) 2009-08-19

Family

ID=18046670

Family Applications (1)

Application Number Title Priority Date Filing Date
JP31388399A Expired - Fee Related JP4316076B2 (en) 1999-11-04 1999-11-04 Composite parts repair equipment

Country Status (1)

Country Link
JP (1) JP4316076B2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4764011B2 (en) * 2005-01-04 2011-08-31 富士重工業株式会社 Repair method for defective parts of composite materials
FR2891193B1 (en) * 2005-09-29 2007-10-26 Airbus France Sas PROCESS FOR THE THREE-SKIN REPAIR OF THREE-SKIN COMPOSITE STRUCTURE AND TWO LAYER LAYERS
DE102007026099A1 (en) * 2007-06-05 2008-12-11 Airbus Deutschland Gmbh Apparatus and method for processing a fiber composite structure
JP4929147B2 (en) * 2007-12-19 2012-05-09 三菱重工業株式会社 How to repair resin products
CN103448264A (en) * 2013-09-06 2013-12-18 杭州顺源轮胎制造有限公司 Tire puncture cut repairing assembly with self-sealing layer and using method of tire puncture cut repairing assembly with self-sealing layer

Also Published As

Publication number Publication date
JP2001129891A (en) 2001-05-15

Similar Documents

Publication Publication Date Title
US5374388A (en) Method of forming contoured repair patches
US6017484A (en) Method for manufacture of minimum porosity, wrinkle free composite parts
JP5721739B2 (en) High temperature composite tool
JP2013514209A5 (en)
JP5728493B2 (en) Method for curing composite parts
US6435242B1 (en) Repair pressure applicator
KR20100017350A (en) Device and method for processing a fibre compound structure
RU2008116590A (en) METHOD AND DEVICE FOR ADHESIVE COMPONENTS TO COMPOSITE FORMED PRODUCT
JP7093299B2 (en) Hot press equipment and metal resin composite molding method
JP4316076B2 (en) Composite parts repair equipment
JPH0629067B2 (en) Device and method for packaging
RU2008126190A (en) METHOD AND DEVICE FOR OBTAINING COMPONENT COMPOUND
JP2014188994A (en) Honeycomb core sandwich panel repair method, and repair apparatus
JPH11207911A (en) Method for molding composite material and molding device
JPS5818902B2 (en) Japanese lily pads
JP2016120711A (en) Installation tool for fitting patch on surface and related method
US20220143935A1 (en) Composite material molding method and composite material molding device
TWI797173B (en) Methods and systems for bonding composite structures
JP2947873B2 (en) Thermosetting resin composite molding method
JP3897511B2 (en) Optical fiber embedding method
FI65769B (en) FOERFARANDE FOER FRAMSTAELLNING AV EN SKIKTAD GLASRUTA
WO2020246001A1 (en) Composite-material molding apparatus and composite-material molding method
JP2729241B2 (en) Laminator for solar cell module
US20220063214A1 (en) Method for manufacturing a composite material part
JP2023061443A (en) Method for bonding composite material

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20061101

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20090417

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20090424

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20090520

R150 Certificate of patent or registration of utility model

Ref document number: 4316076

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120529

Year of fee payment: 3

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20130529

Year of fee payment: 4

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20140529

Year of fee payment: 5

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

S531 Written request for registration of change of domicile

Free format text: JAPANESE INTERMEDIATE CODE: R313531

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

S533 Written request for registration of change of name

Free format text: JAPANESE INTERMEDIATE CODE: R313533

R350 Written notification of registration of transfer

Free format text: JAPANESE INTERMEDIATE CODE: R350

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees